摘要
伴随轨道机动应用相关研究具有重要的应用价值和广阔的应用前景。以仿真研究伴随卫星轨道部署及机动策略为目的，通过对伴随前的机动进入伴随轨道仿真、伴随过程中受摄动因素影响的机动调整仿真和伴随后的机动规避（返回）仿真，研究了伴随卫星执行轨道机动时的速度增量与时间消耗情况，分析了采用不同机动策略达成的机动效果。结果表明：通过伴随轨道机动完成应用任务具有可行性和灵活性。
There are some important application values and wide application prospect of relative research on concomitant orbit maneuver application. The purpose is to simulate and research orbit deploy and maneuver strategy. Phases of concomitant satellite maneuver into concomitant orbit before concomitance, maneuver adjusting under the influence of the perturbation, and maneuver elusion （return） are simulated. The consumption of velocity increment and time of maneuver process are researched, and the various maneuver effects by different maneuver strategies are analyzed. The conclusion is educed that using orbit maneuver in application task is feasible and flexible.
出处
《装备指挥技术学院学报》
2007年第6期109-113,共5页
Journal of the Academy of Equipment Command & Technology
基金
国家高技术发展计划资助项目
关键词
伴随轨道
机动应用
仿真
concomitant orbit
maneuver application
simulation
